DE602005007507D1 - Strahltriebwerkpylon für ein flugzeug - Google Patents

Strahltriebwerkpylon für ein flugzeug

Info

Publication number
DE602005007507D1
DE602005007507D1 DE602005007507T DE602005007507T DE602005007507D1 DE 602005007507 D1 DE602005007507 D1 DE 602005007507D1 DE 602005007507 T DE602005007507 T DE 602005007507T DE 602005007507 T DE602005007507 T DE 602005007507T DE 602005007507 D1 DE602005007507 D1 DE 602005007507D1
Authority
DE
Germany
Prior art keywords
plane
beam power
power pylon
imaginary surface
half rings
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
DE602005007507T
Other languages
German (de)
English (en)
Inventor
Lionel Diochon
Jerome Durand
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE602005007507D1 publication Critical patent/DE602005007507D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Refuge Islands, Traffic Blockers, Or Guard Fence (AREA)
  • Tires In General (AREA)
  • Vibration Dampers (AREA)
DE602005007507T 2004-08-05 2005-08-03 Strahltriebwerkpylon für ein flugzeug Active DE602005007507D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0451791A FR2873988B1 (fr) 2004-08-05 2004-08-05 Mat d'accrochage de turboreacteur pour aeronef
PCT/FR2005/050645 WO2006090032A1 (fr) 2004-08-05 2005-08-03 Mat d'accrochage de turboreacteur pour aeronef

Publications (1)

Publication Number Publication Date
DE602005007507D1 true DE602005007507D1 (de) 2008-07-24

Family

ID=34948383

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005007507T Active DE602005007507D1 (de) 2004-08-05 2005-08-03 Strahltriebwerkpylon für ein flugzeug

Country Status (11)

Country Link
US (1) US7784733B2 (fr)
EP (1) EP1789320B1 (fr)
JP (1) JP4729573B2 (fr)
CN (1) CN100422046C (fr)
AT (1) ATE398074T1 (fr)
BR (1) BRPI0513892A (fr)
CA (1) CA2576100C (fr)
DE (1) DE602005007507D1 (fr)
FR (1) FR2873988B1 (fr)
RU (1) RU2381150C2 (fr)
WO (1) WO2006090032A1 (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2905990A1 (fr) * 2006-09-20 2008-03-21 Snecma Sa Systeme propulsif a pylone integre pour avion.
FR2913664B1 (fr) * 2007-03-16 2009-07-24 Aircelle Sa Nacelle pour turboreacteur double flux
FR2907098B1 (fr) * 2006-10-11 2010-04-16 Aircelle Sa Nacelle pour turboreacteur double flux
US8523516B2 (en) 2006-10-11 2013-09-03 Aircelle Bypass turbojet engine nacelle
FR2917710A1 (fr) * 2007-06-22 2008-12-26 Aircelle Sa Platine de fixation et longeron de manutention d'ensemble propulsif monobloc d'un aeronef
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
FR2929245B1 (fr) * 2008-03-28 2010-05-14 Aircelle Sa Structure primaire d'un mat d'accrochage.
FR2931134B1 (fr) * 2008-05-14 2010-06-18 Airbus France Mat d'accrochage de moteur d'aeronef comprenant un caisson de section en forme de cercle ou d'ellipse
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
FR2939101B1 (fr) * 2008-12-01 2010-12-31 Airbus France Structure rigide de mat d'aeronef plaquee contre une extension laterale de fuselage pour sa fixation
FR2950322B1 (fr) * 2009-09-22 2012-05-25 Airbus Operations Sas Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe
FR2950323B1 (fr) * 2009-09-22 2011-11-04 Airbus Operations Sas Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2993535B1 (fr) * 2012-07-20 2015-03-06 Airbus Operations Sas Ensemble propulsif comprenant un turboreacteur a double flux de tres grand diametre et son dispositif d'accrochage sous la voilure d'un aeronef
US9211955B1 (en) * 2012-12-10 2015-12-15 The Boeing Company Methods and apparatus for supporting engines and nacelles relative to aircraft wings
WO2015010315A1 (fr) 2013-07-26 2015-01-29 Mra Systems, Inc. Mât d'accrochage de moteur pour aéronef
FR3015433B1 (fr) * 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
FR3021029B1 (fr) * 2014-05-16 2016-05-06 Airbus Operations Sas Carenage aerodynamique
FR3021843B1 (fr) * 2014-06-06 2016-07-08 Lesaffre & Cie Methode et composition pour ameliorer la productivite de plantes non legumineuses
US20160167798A1 (en) * 2014-12-12 2016-06-16 General Electric Company Variable pitch mounting for aircraft gas turbine engine
FR3040043B1 (fr) * 2015-08-12 2019-04-12 Sogeclair Sa Mat de moteur d'aeronef a ossature multifonctionnelle integree
US10144525B2 (en) 2015-09-24 2018-12-04 Embraer S.A. Aircraft engine pylon to wing mounting assembly
US9868539B2 (en) * 2015-09-24 2018-01-16 Embraer S.A. Aircraft engine pylon to wing mounting assembly
FR3045570B1 (fr) * 2015-12-16 2017-12-22 Airbus Operations Sas Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe d'une enveloppe structurale fixee sur un caisson central
FR3075174B1 (fr) 2017-12-18 2020-12-11 Safran Aircraft Engines Structure porteuse destinee au montage sur un generateur de gaz
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
FR3115766B1 (fr) * 2020-11-02 2023-03-31 Safran Nacelles Nacelle pour ensemble propulsif d’aéronef, comprenant une bielle de sécurité formant renfort structural
CN114030626B (zh) * 2021-11-30 2024-04-05 北京航星机器制造有限公司 一种不易断裂的挂架、无人机及物品挂载于无人机的方法
US20230182910A1 (en) * 2021-12-13 2023-06-15 Spirit Aerosystems, Inc. Aircraft engine attachment assembly

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666211A (en) * 1970-03-12 1972-05-30 Mc Donnell Douglas Corp Trijet aircraft
US3848832A (en) * 1973-03-09 1974-11-19 Boeing Co Aircraft engine installation
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon

Also Published As

Publication number Publication date
ATE398074T1 (de) 2008-07-15
US20070205324A1 (en) 2007-09-06
JP4729573B2 (ja) 2011-07-20
FR2873988B1 (fr) 2007-12-21
CN1993266A (zh) 2007-07-04
CN100422046C (zh) 2008-10-01
CA2576100A1 (fr) 2006-08-31
US7784733B2 (en) 2010-08-31
RU2007107930A (ru) 2008-09-10
RU2381150C2 (ru) 2010-02-10
BRPI0513892A (pt) 2008-05-20
JP2008509041A (ja) 2008-03-27
EP1789320B1 (fr) 2008-06-11
EP1789320A1 (fr) 2007-05-30
FR2873988A1 (fr) 2006-02-10
WO2006090032A1 (fr) 2006-08-31
CA2576100C (fr) 2013-07-02

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